Analysis of a stability valve system for extending the dynamic range of a supersonic inlet / John A. Webb, Jr., and Miles O. Dustin.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Webb, John A.
Corporate Authors:	Lewis Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Dustin, Miles O.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975.
Series:	NASA technical memorandum ; X-3219.
Subjects:	Airplanes > Motors > Valves > Computer simulation. Airplanes > Turbojet engines > Air intakes > Computer simulation.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:3219
NAS 1.15:3219	Available Place a Hold